The Effect of Blade-Section Thickness Ratios on the Aerodynamic Characteristics of Related Full-Scale Propellers at Mach Numbers up to 0.65

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1953
Accession Number
ADB183080

Entities

People

  • Julian D. Maynard
  • Seymour Steinberg

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeronautical Laboratories
  • Aeronautics
  • Airspeed
  • Efficiency
  • Mach Number
  • Numbers
  • Photographs
  • Propellers
  • Scientific Research
  • Thickness